JASC 2210
Service difficulty reports · 4,019
Reports filed under 2210 · Autopilot System, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2210' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2210' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MASA200400157Controller · smokeFLIGHT GUIDANCE CONTROLLER STARTED SMOKING. MX REPLACED THE GUIDANCE CONTROLLER. OP CHECKS GOOD.SDR 04080669Servo · inoperativeDURING FLIGHT CREW REPORTED AN UNCOMMANDED DISCONNECT OF THE AUTOPILOT SYSTEM. THE ELEVATOR SERVO WAS REPLACED AND IAPS LIGHTING PROTECTION CARD WAS FOUND LOOSE AND TIGHTENED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR SWIA200413056Computer · malfunctionedCAPTAIN'S AUTOPILOT DISENGAGES DUE TO FD FLAG. REMOVED AND REPLACED NR 1 & 2 AUTOPILOT COMPUTERS.SDR MALA040277Computer · malfunctionedAP DISCONNECTED IN CRUISE. FLIGHT WITH THE FOLLOWING SYSTEM FAILURES NOTED: FTC, EL TRIM, YD, AP, MCP/F/D TRP/AUTOTHROTTLES, WITH FGS ADVISORY LIGHTS , FGC1 AND YAW DAMPER. MX REMOVED AND REPLACED FLIGHT GUIDANCE COMPUTER IAW RH AMM 22-10-11-201. REMOVESDR SWIA200413057Computer · malfunctionedWHEN A/P ON CAPTAIN'S SIDE, OCCASIONALLY THE A/P WOULD INITIATE A CLIMB, THEN DESCENT ON ITS OWN. A/P AURAL DID NOT COME ON, SEEMED LIKE AN ELEVATOR FLUCTUATION. REPLACED NR 1 APC-65B IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00. P/N: 622-8315-402, S/N SDR 371PA0039Accessory Unit · malfunctionedAIRCRAFT PITCHES UP AT OR ABOVE .75 MACH WITH AUTOPILOT ENGAGED. REPLACED AFC ACCESSORY UNIT PER MM 22-11-36. OPS CHECKS GOOD.SDR BAQA093829Control Unit · failedYAW CSAS MADE UNCOMMANDED YAW OSCILLATIONS IN NORMAL AND STANDBY MODE AT APPROX. TWO SECOND INTERVALS. UNIT WAS INSTALLED 02/16/2004 AT A/C TT 5145.8 AND WAS REMOVED 03/12/2004 AT A/C TT 5172.2 FOR A TOTAL OF 26.4 HOURS. LAST REPAIR REF RO 9-090006-18 MMIR CLSDR ABXA040107Actuator · bypassingON CLIMBOUT, THE AIRCRAFT EXPERIENCED A VIOLENT LATERAL FLUTTER. THE AUTOPILOT WAS OFF, YAW DAMPER ENGAGED. THE YAW DAMPER WAS DISENGAGED BY PILOT WITH NO NOTEABLE DIFFERENCE. DEPOWERED THE RUDDER HYDRAULICS AND THE FLUTTER STOPPED. FURTHER TROUBLESHOOTINGSDR 2004FA0000352Autopilot Sys · inoperativeIN APR AND NAV MODE, AUTOPILOT WILL NOT PROPERLY INTERCEPT AND TRACK LOCALIZER AND/OR VOR SIGNAL. AUTOPILOT WILL SCALLOP ACROSS COURSE. AUTOPILOT HAS BEEN SENT IN FOR EVALUATION. WE HAVE EVALUATED OUR PN-101 HSI TO DETERMINE IF THEY ARE THE SOURCE. AFTER EVALSDR 371PA0038Coupler · failedYAW DAMPER INOP. PLACED ON MEL 22-03. 03/12/2004: REPLACED YAW DAMPER COUPLER PER MM 22-13-31 PG 401. TESTS OK.SDR SWIA200413013Control Panel · malfunctionedAUTO PILOT, EITHER SIDE, WILL NOT HOLD ALTITUDE. REPLACED APP-65 WITH A SERVICEABLE UNIT. OPS CHECK GOOD.SDR 757BJ0007Computer · failedFIRST OFFICER'S FLIGHT DIRECTOR BARS WENT ERRATIC IN CRUISE (INTERMITTENT). REPLACED RIGHT FCC COMPUTER PER MM 22-11-01. CHECKED BAD UPON INSTALLATION. REMOVED FCC COMPUTER, CLEANED AND RERACKED ORIGINAL FCC COMPUTER PER MM 22-11-01. OPS CHECKED OK.SDR 371PA0037Computer · malfunctionedMACH TRIM INOP. UNABLE TO DUPLICATE. PERFORMED ALL MACH TRIM TESTS PER MM 22-11-01. PREVIOUS FAULTS FLAGGED NR 1 FCC. REPLACED NR 1 FCC PER MM 22-11-33 FOR TROUBLESHOOTING. OPS CHECKS GOOD.SDR 2004FA0000300Bridal Cable · wornROLL SERVO BRIDLE CABLE WAS IMPROPERLY INSTALLED. TOP PORTION OF CABLE WAS WRAPPED AROUND PRIMARY AILERON CABLE, CAUSING BRIDLE CABLE TO CHAFE AGAINST A PULLEY FLANGE. INSTALLATION OF CABLE ASSEMBLY OCCURRED AT THE FACTORY AND HAS NOT BEEN REPLACED SINCE AIRSDR SWIA200413002Control Panel · malfunctionedFD FLAG CAPTAIN SIDE. REPLACED CONTROL PANEL (FCP65) IAW 22-10-03. OPS CHECKS GOOD.SDR 251TR0007Display · malfunctionedTHE NUMBER 6 IS MISSING IN MODE CONTROL PANEL. PLACED ON MCO. 3/9/2004: REPLACED MODE CONTROL PANEL AND OPS CHECKED PER MM 22-11-341.SDR SWIA200412987Computer · malfunctionedWHEN SELECTING AUTOPILOT TO FIRST OFFICER'S SIDE, THE TRIM FAILS WITH ALL ASSOCIATED WARNINGS. RERACKED NR 2 AUTOPILOT COMPUTER. OPS CHECKS GOOD.SDR 234TR0016Computer · malfunctionedMCP AUTOPILOT B INOP AND F/O FLIGHT DIRECTOR INOP. PLACED ON MEL 22-15-2.SDR 251TR0006Warning Horn · inoperativeAUTO PILOT DISCONNECT AURAL WARNING INOP. MECHANIC STATED THAT WHEN HE ARRIVED IN CONTROL CABIN, THE AURAL WARNING C/B WAS OUT. THE C/B WAS RESET AND AN OPERATIONAL CHECK OF THE AURAL WARNING PERFORMED SATISFACTORILY PER MM 22-11-01. THERE HAVE BEEN NO FURTHERSDR MALA040221Computer · malfunctionedFTC/EL TRIM LIGHT ILLUMINATED DURING TAKEOFF ROLL. AIR RETURN TO MSP. REPLACED FGC. TESTS GOOD IAW AVRO MM CH 22.SDR 234TR0015Control Panel · malfunctionedCOPILOT COURSE SELECTOR ON MCP WILL NOT ALLOW YOU TO SELECT 122 DEGREES. REPLACED MCP PER MM 22-11-341 AND OPS CHECKED.SDR SWIA200412956Spring · damagedCAPTAIN AP/TRIM INOP. REPLACED CAPTAIN'S YOKE RETURN SPRING WITH A SERVICEABLE SPRING. CAPT'S AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00.SDR 757BJ0006Control Panel · intermittentAFCS MODE CONTROL PANEL HAS INTERMITTENT FAILURE, RT SIDE, A/SPEED BUG GOES TO 300-350 WITHOUT COMMAND. REPLACED AFCS MODE CONTROL PANEL WITH SERVICEABLE UNIT PER MM 22-11-02.SDR SWIA200412947Switch · dirtyCLIMBING OUT OF SLC, AUTOPILOT WOULD NOT ENGAGE ON EITHER CAPT'S OR F/O'S SIDE. F/O'S WORKED BOTH SIDES. NO WARNING OR CAUTION MESSAGE DISPLAYED. CLEANED AUTOPILOT DISENGAGE SWITCHES. OPS CHECKS GOOD.SDR SWIA200412983Computer · malfunctionedDURING FLIGHT, CAPTAIN'S ADI AND FLIGHT DIRECTOR WERE ERRATIC CAUSING A COMPUTER FAILURE AND THE A/P TO DISENGAGE. INSTALLED SERVICEABLE APC-65B ON THE CAPTAIN'S SIDE IAW EMB 120 MM CHAPTER 22-10-02. OPS CHECK GOOD.SDR SWIA200412941Warning Light · intermittentYD-2 MESSAGE APPEARS AND RESETS MOMENTARILY THEN DISENGAGES. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR PER WW 22-22-01. OPS CHECK GOOD.SDR 21200004Autopilot Sys · defectiveAIRCRAFT PORPOISES WHILE IN ALTITUDE HOLD MODE. DISABLE ALTITUDE HOLD MODE. MAINTENANCE CONFIRMS DEFECTIVE UNIT BY MANUFACTURER. MANUFACTURER UNABLE TO SUPPLY REPLACEMENT PART.SDR SWIA200412934Pin · brokenF/O'S ELECTRIC TRIM NOSE UP INOP. REPAIRED BROKEN PIN ON J2 PIN 1. RERACKED APC NR 2. OPS CHECK GOOD IAW MM 22-10-00.SDR 737DX0003Limiter · malfunctionedAILERON FORCE LIMITER FAILED LRU INTERFACE TEST 50 PERCENT OF THE TIME. REPLACED AILERON FORCE LIMITER PER MM 22-11-13. OPS CHECKS GOOD PER MM 22-11-13.SDR 2004FA0000204Autopilot Sys · malfunctionedONCE ESTABLISHED IN CRUISE FLIGHT WITH ALTITUDE HOLD ENGAGED, THE S-TEC SYSTEM 55X AUTOPILOT FREQUENTLY BEGINS TO GENTLY PORPOISE IN PITCH. THIS GETS PROGRESSIVELY WORSE UNTIL THE AUTOPILOT CAUSES SERIOUS PITCH EXCURSIONS OF SEVERAL HUNDRED FEET PER MINUTE UPSDR GAIA04030OPCoupler · damagedDURING TAXI, THE UPPER YAW DAMPER WAS CAUSING THE RUDDER TO SWING SIDE TO SIDE CAUSING VIBRATION. REMOVED AND REPLACED THE UPPER YAW DAMPER COUPLER. OPERATIONAL CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR BAQA093101Actuator · inoperativeTRIM ACTUATOR UNIT PITCH AUTO TRIM DECOUPLES. SELF TEST FAULT CODE 1. REPLACED WITH SERVICABLE UNIT. 02/23/2004SDR 371PA0036Actuator · malfunctionedDURING LEVEL CRUISE WITH AUTOPILOT A OR B ENGAGED, AIRCRAFT OCCASIONALLY GAINED 150 FT ALTITUDE WHILE ALTITUDE HOLD MODE ENGAGED. REPLACED MACH TRIM ACTUATOR PER MM 22-21-11.SDR SWIA200412924Computer · malfunctionedDURING CLIMBOUT YAW DAMPER 2 DISENGAGED AND WOULD RESET FOR 2 TO 5 MINUTES AND THEN DISENGAGE. REMOVED AND REPLACED FCC 2 IAW 22-12-14. OPS CHECK GOOD.SDR BAQA092697Light · inoperativeSEVERAL LIGHTS INOPERATIVE ON UNIT. MRA NR 1155272-000020 REPLACED WITH SERVICABLE UNIT. 02/16/2004SDR SWIA200412889Computer · malfunctionedCAPTAIN'S AUTOPILOT WILL CLIMB AND DESCEND 100 FT WHEN IN LEVEL FLIGHT. SWITCHED TO F/O'S AUTOPILOT. NO DISCREPANCIES. COULD NOT DUPLICATE. REPLACED NR 1 APC FOR TROUBLESHOOTING SYSTEM. OPS CHECKS GOOD IAW 22-10-00.SDR 304AW0003Relay · stickingCREW REPORTED THAT THE AUTOPILOT COMMAND-A WILL NOT ENGAGE UNLESS COMMAND-B IS ENGAGED FIRST. REPLACED AILERON FORCE LIMITER CLUTCH RELAY DUE TO STICKING. CHECKS OK PER MM 22-11-13.SDR GAIA04027OPAutopilot Sys · malfunctionedFLT 278 - SFO-FWA - DUIRNG CRUISE HAD TO KEEP AUTO PILOT TURN KNOB ALL THE WAY TO THE LEFT TO HAVE AIRPLANE FLY STRAIGHT AND LEVEL. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED AUTOPILOT SYSTEM OPS CHECKS ON GROUND. COULD NOT DSDR BAQA092611Module · failedTRIM ACTUATOR MODULE WILL NOT TURN ON, OR TEST. 3 SLASHES ON PFD INDICATING MASSIVE FAILURE OF APM. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/10/2004SDR BAQA092533Actuator · intermittentPITCH ACTUATOR INTERMITTENT KICK OFF. OFF PITCH LANES. REPLACED WITH SERVICEABLE ASSET UNIT. 02/26/2004SDR SWIA200412864Actuator · disconnectedYAW DAMPER NR 1 WOULD NOT RESET AFTER IT DISCONNECTED. REPLACED NR 1 YAW DAMPER WITH SERVICEABLE UNIT. OPS CHECKS GOOD.SDR SWIA200412881Connector · dirtyFIRST OFFICER'S AUTOPILOT FAILED WITH ASSOCIATED AUTOPILOT FAIL ON MAP AND T, A, R, E ON AUTOPILOT PANEL. INSPECTED AND CLEANED F/O'S AP COMPUTER RACK AND CONNECTORS, AP CONTROL PANELS AND AHRS COMPUTER CONNECTORS. TROUBLESHOT THE F/O'S AP SYSTEM. NO FAULTSSDR SWIA200412863Computer · malfunctionedCAPTAIN AUTOPILOT FAILED, -E- ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED NR 1 APC-65 WITH SERVICEABLE UNIT IAW MM 22-10-00. OPS CHECK GOOD AT THIS TIME.SDR 2004F00088Actuator · inoperativeBLUE YAW DAMPER, FAIL LOWER 'B' CAS MESSAGE, AMBER YAW DAMPER OFF LOWER CAS MESSAGE AND PRI STAB TRIM FAIL AND MACH TRIM OFF CAS MESSAGE CAME ON DURING FLIGHT. CHANNEL 'B' YAW DAMP ACTUATOR FAILED TO OPERATE. REPLACED CHANNEL 'B' YAW DAMP ACTUATOR. OPERATIOSDR X072004F00000Actuator · inoperativePILOTS FOUND AILERON SYSTEM ROUGH ON PREFLIGHT. MECHANICS IN CHECKING OUT CAUSE, FOUND AILERON SYSTEM TO LOCKUP AND WOULD NOT FREE UP UNTIL SERVO WAS REMOVED. APPEARS BEARING IN GEAR BOX IS SLOPPY AND GEAR WILL BIND UP WHEN TURNED.SDR SWIA200412841Control Panel · malfunctionedCAPTAIN SIDE AUTOPILOT FAILS WHEN ENGAGED EN ROUTE. FD OPERATES NORMALLY BUT AP DSC FLAG AND AP ERROR LIGHT APPEAR ON FCP AND AP CONTROL PANEL INDICATES AP DIS AND RED AP LIGHT AND AMBER FLAG ERRORS. REMOVED AND REPLACED AP CONTROL PANEL WITH NEW CONTROL PANSDR SWIA200412843Computer · malfunctionedCREW REPORTS NR 1 AUTOPILOT WON'T CAPTURE HDG. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00.SDR QXEA200400099Warning Light · illuminatedBIL- ON FLIGHT 2508 AFTER TAKEOFF AUTOPILOT TRIM IS SHOWING A CAUTION MESSAGE. DISCONNECTED AUTOPILOT, RETRIMMED, THEN RECONNECTED PER CHECKLIST. NO FURTHER INCIDENTS. COMPLIED WITH AUTOPILOT SYSTEM OPERATIONAL CHECK IAW CRJ AMM 22-11-00-710-802 AND 22-11-2SDR SWIA200412819Computer · malfunctionedAFTER POWER UP DURING ORIGINATING CHECKS, THE YD2 INOP. MESSAGE AND FD2 FAIL MESSAGE ILLUMINATED AND COULD NOT BE REMOVED. REMOVED AND REPLACED NR 2 FCC CARD IAW AMM CHAPTER 22-12-14. OPS CHECK GOOD.SDR SWIA200412817Computer · malfunctionedAUTO PILOT AURAL WARNING AND TRIPLE CHIME WHEN SELECTED TO F/O SIDE. INSTALLED SERVICEABLE APC-65. OPS CHECK GOOD. S/N OFF: 2736.
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